WO2019193269A1 - Procede et systeme d'emission et de reception d'impulsions laser - Google Patents

Procede et systeme d'emission et de reception d'impulsions laser Download PDF

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Publication number
WO2019193269A1
WO2019193269A1 PCT/FR2019/050719 FR2019050719W WO2019193269A1 WO 2019193269 A1 WO2019193269 A1 WO 2019193269A1 FR 2019050719 W FR2019050719 W FR 2019050719W WO 2019193269 A1 WO2019193269 A1 WO 2019193269A1
Authority
WO
WIPO (PCT)
Prior art keywords
pulses
transmitting
reception
received
laser
Prior art date
Application number
PCT/FR2019/050719
Other languages
English (en)
French (fr)
Inventor
Guy-Maël JACOBE DE NAUROIS
David PARRAIN
Bruno Esmiller
Original Assignee
Arianegroup Sas
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Arianegroup Sas filed Critical Arianegroup Sas
Priority to ES19719560T priority Critical patent/ES2967662T3/es
Priority to CA3095903A priority patent/CA3095903A1/fr
Priority to EP19719560.5A priority patent/EP3759518B1/de
Priority to US17/044,444 priority patent/US20210033705A1/en
Publication of WO2019193269A1 publication Critical patent/WO2019193269A1/fr

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Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S17/00Systems using the reflection or reradiation of electromagnetic waves other than radio waves, e.g. lidar systems
    • G01S17/02Systems using the reflection of electromagnetic waves other than radio waves
    • G01S17/06Systems determining position data of a target
    • G01S17/08Systems determining position data of a target for measuring distance only
    • G01S17/10Systems determining position data of a target for measuring distance only using transmission of interrupted, pulse-modulated waves
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/483Details of pulse systems
    • G01S7/486Receivers
    • G01S7/487Extracting wanted echo signals, e.g. pulse detection
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01SRADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S7/00Details of systems according to groups G01S13/00, G01S15/00, G01S17/00
    • G01S7/48Details of systems according to groups G01S13/00, G01S15/00, G01S17/00 of systems according to group G01S17/00
    • G01S7/483Details of pulse systems
    • G01S7/486Receivers
    • G01S7/487Extracting wanted echo signals, e.g. pulse detection
    • G01S7/4876Extracting wanted echo signals, e.g. pulse detection by removing unwanted signals

Definitions

  • the present invention relates to a method and a system for transmitting and receiving laser pulses.
  • a system for transmitting and receiving laser pulses may be part of a high frequency laser rangefinder which is particularly intended for use in various applications in the space field.
  • Such a laser rangefinder can, in particular, be used to implement a laser tracking or laser telemetry satellite type SLR (for "Satellite Laser Ranging” in English).
  • SLR for "Satellite Laser Ranging” in English.
  • a system for transmitting and receiving laser pulses at high frequency is to provide a communication laser link between a ground station and a drone (or an object or machine in orbit). using a technology of modulated retro-reflectors.
  • the laser system is provided in the ground station for emitting a laser beam for illuminating a retro-reflector mounted on the drone (or on the object or machine in orbit).
  • This retro-reflector is designed to modulate the reflected intensity. It is constructed (in the form of a cube corner or a spherical reflector for example) so that the laser beam is reflected exactly in the same direction as that of the received laser beam.
  • the modulation is detected and processed by the ground system.
  • Other applications are also possible for such a system for transmitting and receiving laser pulses.
  • the object of the present invention is to remedy these drawbacks by proposing a method for transmitting and receiving laser pulses making it possible to increase the firing rate (and thus the probability of detection).
  • said method for transmitting and receiving laser pulses comprises at least the following steps:
  • a step of generating at least one pulse pattern implemented by a generation unit, said pulse pattern comprising at least three successive pulses, two successive pulses of said pulse pattern being each temporally separated; an associated separation time, the different separation times of the pulse pattern being variable and conform to a given model;
  • a transmission step implemented by a transmitting / receiving unit, consisting in transmitting at least one set of pulses comprising a sequence of laser pulses according to said pulse pattern and recording at least the said time; emission time, at which the first pulse of the laser pulse sequence of said set of pulses is transmitted; a reception step, implemented by the transmitting / receiving unit, consisting in receiving light pulses and recording said reception time times at which these light pulses are received; and
  • an analysis step carried out by a data processing unit, consisting at least of analyzing the durations between the reception times of the light pulses received at the reception step in order to identify a sequence of light pulses received, which conforms to said impulse pattern.
  • the analysis step consists in deducing, from the identified sequence of pulses, a so-called reception time at which the first pulse of said identified sequence of pulses is received, and calculating the duration between said time of transmission and said reception time.
  • the pulses of a set formed by a plurality of pulses by defining (temporally) the durations between, in each case, two successive pulses for make them unique within the set of pulses according to said impulse pattern.
  • sets (or packets) of pulses in the form of a so-called "burst" or burst transmission mode
  • burst or burst transmission mode
  • the method for transmitting and receiving laser pulses thus makes it possible, in particular, to reduce the energy of each emitted laser pulse (for example up to 10 ⁇ J), to distribute it in several laser pulses (forming the set of pulses) and temporally sign these laser pulses (according to the pulse pattern). This makes it possible to transmit at a higher rate of fire to improve the probability of detection, while keeping a high emission accuracy in the case in particular of telemetry, and maintaining a low average energy, which is favorable to eye safety.
  • the analysis step consists in determining, by means of said duration between the transmission time and the reception time, a distance between a station comprising the transmission / reception unit. and an object (or target) receiving the transmitted laser pulses and returning them.
  • the analysis step consists of analyzing at least one set of transmitted pulses and the corresponding sequence of received pulses, resulting for example from modulation and retro-reflection. , to deduce information, for example in the context of a laser communication link with a drone or an object in orbit in space.
  • the analysis step consists in correlating said pulse pattern with the light pulses received on a correlation window to identify the sequence of received light pulses, which is consistent with said pattern of pulses. pulses.
  • the transmitting step consists in emitting, successively, a plurality of sets of pulses.
  • the duration between two sets of pulses emitted successively is greater than a round trip time of a set of pulses between a station comprising the transmission / reception unit and an object receiving the laser pulses emitted and returning them.
  • the generation step consists in generating at least two different pulse patterns and the transmitting step consists in transmitting a plurality of successive pulse sets which are in accordance with different pulse patterns generated in the generation step.
  • the present invention also relates to a system for transmitting and receiving laser pulses, comprising a transmitting / receiving unit.
  • said system for transmitting and receiving laser pulses comprises:
  • a generation unit configured to generate at least one pulse pattern, said pulse pattern comprising at least three successive pulses, two successive pulses of said pulse pattern being each time separated by an associated separation time, the different separation times of the pulse pattern being variable and conform to a given model;
  • the transmitting / receiving unit which is configured to:
  • At least one memory configured to record at least so-called reception times, to which the light pulses are received by the transmitting / receiving unit;
  • a data processing unit configured at least for analyzing the times between the reception times of the light pulses to identify a sequence of received light pulses, which is in accordance with said pulse pattern.
  • said memory is configured to record also a so-called transmission time, which is emitted the first pulse of the laser pulse sequence of said set of pulses emitted by the transmitting / receiving unit.
  • the data processing unit is also configured for:
  • said system for transmitting and receiving laser pulses also comprises at least one filter unit configured to perform at least one frequency filtering of the received light pulses, relative to the frequency or frequencies of the laser pulses emitted. .
  • the present invention further relates to a laser range finder and / or a communication system, comprising a laser pulse emission and reception system, such as that described above.
  • FIG. 1 is the block diagram of a particular embodiment of a laser pulse emission and reception system according to the invention
  • FIG. 2 is a schematic view of a three-pulse pulse pattern
  • FIG. 3 schematically shows two superimposed graphs making it possible to explain the operation of a transmission / reception unit of a laser pulse emission and reception system
  • FIGS. 4 to 7 schematically illustrate different successive steps of a correlation analysis, with a view to identifying a sequence of received light pulses, which is in accordance with a pattern of pulses with four pulses;
  • FIG. 8 is a block diagram of a method for transmitting and receiving laser pulses.
  • FIG. 1 shows a system for transmitting and receiving laser pulses (hereafter "system 1") at high frequency, which is shown schematically in a particular embodiment.
  • system 1 a system for transmitting and receiving laser pulses
  • This system 1 which is mounted on a station 2, installed for example on the ground, can be used in many applications, as indicated above.
  • the system 1 can also be mounted on a land, sea or air machine (not shown).
  • the system 1 comprises a transmitting / receiving unit 3.
  • the transmitting / receiving unit 3 comprises, as represented in FIG.
  • a transmission module 4 configured to emit laser pulses, via optical 5 (transmission / reception), for example laser pulses with a duration of the order of 0.3 ns;
  • a receiving module 6 configured to receive (or detect) light pulses, including laser pulses via the optics 5 (transmission / reception).
  • said system 1 further comprises, as shown in Figure 1, a generation unit 7 which is configured to generate at least one pattern of pulses.
  • the generation unit 7 comprises, for example, means allowing an input operator characteristics of the pulse pattern or means for automatically defining these characteristics.
  • a pulse pattern comprises, as shown for a pulse pattern M1 in FIG. 2, at least three successive pulses I namely the pulses 11, I2 and I3 on the example of FIG. FIG. 2.
  • the pulse pattern used by the system 1 may also comprise more than three successive pulses, for example four pulses 11, I2, I3 and I4 as the pulse pattern M2 of Figures 4 to 7, or more than four pulses.
  • Two directly successive impulses of the pulse pattern are each temporally separated by an associated separation time, namely in the example of FIG. 2 a separation time T1 between the pulses 11 and I 2 of a duration separating T2 between pulses I2 and I3, and in the example of FIG. 4 with more than one separation time T3 between pulses I3 and I4.
  • the different separation times T1, T2 and T3 of the pulse patterns M1 and M2 are variable, that is to say different from one another, and conform to a given model (of separation times), i.e., each separation time is equal to a particular duration.
  • the pulse pattern therefore represents a signature (temporal) of the pulses considered.
  • the transmission module 4 of the transmitting / receiving unit 3 is configured to emit at least one set of pulses EU comprising a sequence of laser pulses, in accordance with the considered pulse pattern, as represented in FIG.
  • the set UE comprises the sequence of pulses 11, I 2, I 3 and I 4 (which are transmitted by being separated temporally according to the pattern of pulses M2).
  • the reception module 6 of the transmitting / receiving unit 3 is configured to receive light pulses ILi (FIG. 3).
  • the reception module 6 receives, for example, pulses corresponding to noises, and also the laser pulses which have been:
  • This object 9 is preferably a moving object in the sky, for example a drone or a satellite (or any other object) in orbit. This object 9 can be located at a high distance from the station 2, for example a few tens of kilometers from the station 2.
  • the system 1 also comprises, as represented in FIG. 1, at least one memory 11 which is configured to record:
  • the time (or moment) said transmission time tE which is emitted at least the first pulse 11 of the sequence of laser pulses of said set of pulses EU emitted by the transmission module 4, as shown in the graph at the top of FIG. 3.
  • This graph illustrates the emissions E1 of pulses (made by the transmission module 4) as a function of time t.
  • the sets of pulses EU conform to the pulse pattern M2 of FIGS. 4 to 7;
  • the transmission module 4 is controlled so as to emit, successively, a plurality of sets of pulses EU.
  • the successive transmissions are separated, each time, by a so-called firing (or emission) duration TR, that is to say that the emissions of the first pulses 11 of two sets UE emitted successively are separated from said duration TR.
  • the system 1 further comprises a data processing unit 12.
  • the data processing unit 12 comprises, as shown in FIG. 1, a processing element 13 which is configured to analyze the durations between the reception times. tRi of the different light pulses ILi received by the reception module 6, to identify a sequence of light pulses received, which is in accordance with the pulse pattern used.
  • the reason The pulse sequence used by the transmission module 4 is, for example, stored in the memory 11.
  • the sequence of pulses identified by the processing element 13 is such that the reception times tRi of the light pulses ILi of this sequence light pulses are separated from each other by separation times which are identical, with a margin, to the separation times T1 to T3 of the pulse pattern used, and this in the same order of appearance.
  • the processing element 13 is configured to make a correlation between the used pulse pattern M2 and the received light pulses ILi, on a correlation window F, to identify the sequence of light pulses received, which is in accordance with said pulse pattern M2, as shown in FIGS. 4 to 7.
  • the pulse pattern M2 (four pulses in this example) is moved, as illustrated by arrow A in FIGS. 4 and 5, and for each successive group of four successive pulses ILi received, processing element 13 checks whether the durations between these four light pulses ILi (which are obtained from the corresponding reception times tRi) correspond to the separation times T1 to T3 of the pulse pattern M2.
  • FIGS. 4 to 7 it is indicated on a graph provided in the lower part of these figures, the number N of correspondences obtained for each correlation, that is to say for each successive group of four pulses.
  • the correlation makes it possible to identify a series of pulses whose first pulse is located at a position P in FIG. 7, the position P being associated with the highest number N of the correlation.
  • the system 1 is able to differentiate, between them, the pulses of a set EU from a plurality of pulses by defining (temporally) the durations between, in each case, two successive (or consecutive) pulses for the make them unique within the pulse set EU, in accordance with the pulse pattern M1, M2 used. Consequently, the system 1 can transmit EU sets (or packets) of pulses (in the form of a so-called "burst" or burst transmission mode), knowing that it will be able to identify the receiving the set of transmitted (and returned) pulses, and in particular determining the reception time at which the first pulse of said set of pulses thus identified is received.
  • the data processing unit 12 also comprises, as shown in FIG. 1, a processing element 14.
  • This processing element 14 is configured:
  • the data processing unit 12 comprises a processing element 15.
  • the processing element 15 thus implements a telemetry function, by measuring the distance between the station 2 and the object 9.
  • the data processing unit 12 comprises a processing element 16.
  • This processing element 16 is configured to analyze at least one set of pulses EU emitted and the sequence of pulses (received) corresponding. This sequence of pulses results, for example, from a modulation and a retro-reflection carried out on the object 9. From this analysis, the processing element 16 is able to deduce, in the usual way , various information.
  • This particular embodiment may, for example, be used in the context of a communication laser link between the station 2 and the object 9, for example a drone or an object orbiting in space.
  • the firing time TR (between two sets of successively transmitted pulses EU) is greater than a round trip time of a set of laser pulses between the station 2 comprising the transmission / reception unit 3 and the transmission unit. object 9 receiving the laser pulses emitted and returning them.
  • this round trip time can be between 1 and 5 milliseconds.
  • the data processing unit 12 can transmit the results of its processing, for example the distance calculated by the processing element 15 and / or the information deduced by the processing element 16, to a user system (not represented). via a link 19.
  • the generation unit 7 is configured to generate at least two different pulse patterns
  • the transmission module 4 is configured to transmit a plurality of successive pulse sets which are consistent with these different pulse patterns, generated by the generation unit 7.
  • the processing operations performed by the given processing unit 12 are similar to those mentioned above, simply taking into account the difference between the pulse patterns used.
  • the generation unit 7, the memory 11 and the data processing unit 12 form part of a central unit 17 of the system 1.
  • the system 1 also comprises at least one filtering unit 18, preferably part of the transmission / reception unit 3.
  • the filtering unit 18 is configured to carry out filtering, and at least one filtering frequency of the light pulses detected by the reception module 6, to keep (for processing by the data processing unit 12) only the detected light pulses which have frequencies located in defined areas around the frequency or frequencies laser pulses emitted by the transmission module 4.
  • the system 1 (laser pulse emission and reception), as described above, is very advantageous.
  • it makes it possible to reduce the energy of each laser pulse (for example up to 10 ⁇ J), to distribute the energy in several laser pulses (forming the set of pulses EU) and to temporally sign these pulses (in accordance with FIG. the impulse pattern considered, for example M1 or M2).
  • This makes it possible to transmit at a higher TR firing rate to improve the probability of detection, while maintaining the precision required in case of telemetry, and by maintaining a low average energy of the laser pulses emitted, which is advantageous in terms of eye safety.
  • the resolution can be increased by increasing the number of pulses and / or decreasing the size of the correlation window F.
  • the system 1 is capable of implementing a method for transmitting and receiving high frequency laser pulses.
  • This method of transmitting and receiving laser pulses comprises, as shown in FIG. 8 (in connection with FIG. 1), the following steps:
  • a generation step E1 implemented by the generation unit 7, to generate a pulse pattern M1, M2 comprising at least three successive pulses;
  • a transmission step E2 implemented by the transmission module 4 of the transmission / reception unit 3, consisting in transmitting at least one set of pulses EU and preferably a plurality of sets of pulses EU, a set of pulses EU comprising a series of laser pulses according to said pattern of pulses used, and to record (in the memory 11) the time (or moment) said transmission time tE, which is emitted the first pulse 11 of said set of pulses EU;
  • a reception step E3 implemented by the reception module 6 of the transmission / reception unit 3, consisting of receiving light pulses ILi and recording the so-called reception time times tRi at which these light pulses ILi are received;
  • an analysis step E4 implemented by the data processing unit 12, consisting of analyzing at least the durations between the reception times tRi of the light pulses ILi received by the reception module 6, to identify a sequence of received light pulses, which conforms to the pulse pattern M1, M2 used during transmission.
  • the analysis step E4 performs a correlation, implemented by the processing element 13, between said pulse pattern M1, M2 and the received light pulses ILi, on a correlation window F, for identifying a sequence of received light pulses, which is in accordance with said M1, M2 pulse pattern.
  • the analysis step E4 also consists in deducing, from the sequence of pulses thus identified, a so-called reception time tR at which the first pulse 11 of said identified sequence of pulses is received, and calculating the duration T0 between said transmission time tE and said reception time tR.
  • the analysis step E4 consists of determining, using the duration T0 (thus calculated) between the transmission time tE and the reception time tR, a distance D0 between the item 2 comprising the transmitting / receiving unit 3 and the object 9 having received the transmitted laser pulses and having sent them back.
  • the analysis step E4 may consist of analyzing at least one set of transmitted pulses and the corresponding sequence of received pulses, resulting for example from a modulation and a retro-reflection, for derive information, for example in the context of a communication laser link.
  • a system 1 transmission and reception of laser pulses
  • terrestrial, maritime and / or aerial (or space) applications with in particular long-range transmissions (greater than ten kilometers).
  • the system 1, as described above, is part of a high frequency laser range finder (not shown) that can be used in a variety of space applications.
  • the range finder uses in particular the distance between the item 2 (of measurement) and the object 9, as determined by the processing element 15 of the data processing unit 12.
  • Such a laser rangefinder can, in particular, be used to implement a laser tracking via laser satellite telemetry (SLR type for "Satellite Laser Ranging"), in particular to very precisely determine the orbits of space objects (satellites, debris).
  • SLR laser satellite telemetry
  • the system 1 illuminates a retro-reflector mounted on the object 9.
  • This retro-reflector is designed to modulate the reflected intensity. It is realized, for example in the form of a cube corner or a spherical reflector, so that the returned laser pulse is reflected exactly in the same direction as that of the received laser pulse.
  • the modulation is detected and processed by the system 1, for example using the processing element 16, to deduce the corresponding information.
  • the system 1 can also be used, in another application, to implement active locking of very long-range targets.

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  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Computer Networks & Wireless Communication (AREA)
  • General Physics & Mathematics (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Electromagnetism (AREA)
  • Optical Radar Systems And Details Thereof (AREA)
PCT/FR2019/050719 2018-04-03 2019-03-28 Procede et systeme d'emission et de reception d'impulsions laser WO2019193269A1 (fr)

Priority Applications (4)

Application Number Priority Date Filing Date Title
ES19719560T ES2967662T3 (es) 2018-04-03 2019-03-28 Procedimiento y sistema de emisión y de recepción de pulsos láser
CA3095903A CA3095903A1 (fr) 2018-04-03 2019-03-28 Procede et systeme d'emission et de reception d'impulsions laser
EP19719560.5A EP3759518B1 (de) 2018-04-03 2019-03-28 Verfahren und system zum aussenden und empfangen von laserimpulsen
US17/044,444 US20210033705A1 (en) 2018-04-03 2019-03-28 Method and system for emitting and receiving laser pulses

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1800272A FR3079619B1 (fr) 2018-04-03 2018-04-03 Procede et systeme d'emission et de reception d'impulsions laser
FR1800272 2018-04-03

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WO2019193269A1 true WO2019193269A1 (fr) 2019-10-10

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PCT/FR2019/050719 WO2019193269A1 (fr) 2018-04-03 2019-03-28 Procede et systeme d'emission et de reception d'impulsions laser

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US (1) US20210033705A1 (de)
EP (1) EP3759518B1 (de)
CA (1) CA3095903A1 (de)
ES (1) ES2967662T3 (de)
FR (1) FR3079619B1 (de)
WO (1) WO2019193269A1 (de)

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WO2023229916A1 (en) * 2022-05-27 2023-11-30 Chevron U.S.A. Inc. Iterative well log depth shifting

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US20220262262A1 (en) * 2021-02-18 2022-08-18 Honeywell International Inc. Vehicle traffic control communication system

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US20120257186A1 (en) * 2011-04-07 2012-10-11 Riegl Laser Measurement Systems Gmbh Method for Measuring Distances
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CN110573900A (zh) * 2017-01-05 2019-12-13 图达通爱尔兰有限公司 用于编码和译码LiDAR的方法和系统
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EP2157445A2 (de) * 2008-08-19 2010-02-24 Rosemount Aerospace Inc. Lidar-System mit Pseudozufallsimpulsfolge
US20120257186A1 (en) * 2011-04-07 2012-10-11 Riegl Laser Measurement Systems Gmbh Method for Measuring Distances
US20160327646A1 (en) * 2015-05-07 2016-11-10 GM Global Technology Operations LLC Pseudo random sequences in array lidar systems

Cited By (2)

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Publication number Priority date Publication date Assignee Title
WO2023229916A1 (en) * 2022-05-27 2023-11-30 Chevron U.S.A. Inc. Iterative well log depth shifting
US20230400598A1 (en) * 2022-05-27 2023-12-14 Chevron U.S.A. Inc. Iterative well log depth shifting

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Publication number Publication date
ES2967662T3 (es) 2024-05-03
FR3079619A1 (fr) 2019-10-04
EP3759518A1 (de) 2021-01-06
CA3095903A1 (fr) 2019-10-10
US20210033705A1 (en) 2021-02-04
EP3759518B1 (de) 2023-10-11
FR3079619B1 (fr) 2020-09-25
EP3759518C0 (de) 2023-10-11

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